View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 59U 60013B 25137.93338112 .00000141 00000-0 65293-4 0 9997
2 59 28.2516 354.4558 0189032 237.4124 120.8040 13.53137866190468
| Epoch (UTC): | 17 May 2025 22:24:04 |
| Eccentricity: | 0.0189032 |
| inclination: | 28.2516° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 354.4558° |
| argument of perigee: | 237.4124° |
| revolutions per day: | 13.53137866 |
| mean anomaly at epoch: | 120.8040° |
| orbit number at epoch: | 19046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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